Embraer EMB145 - Page 814

FLIGHT PLANNING
EMB-145 A1 and A1P LB
AIRPLANE
OPERATIONS
MANUAL
1-05-15
Page
8
Code
02
REVISION 40
AOM-145/1114
LONG RANGE CRUISE - ALL ENGINES OPERATING
AE3007A1 AND AE3007A1P ENGINES
ALTITUDE : 19000 FT TO 28000 FT
CRUISE CONFIGURATION
BLEED: OPEN
ISA CONDITION
WEIGHT ALTITUDE (FT)
(LB)
19000 20000 21000 22000 23000 24000 25000 26000 27000 28000
N1 % 72.8 73.5 74.3 75.1 75.9 76.8 77.7 78.5 79.2 79.9
F FLOW LB/H/ENG 1055 1049 1045 1041 1038 1035 1034 1029 1028 1027
IAS KT 235 234 233 232 231 231 230 229 228 228
42000 TAS KT 312 315 319 323 327 331 335 339 345 350
INDICATED MACH 0.505 0.513 0.521 0.53 0.539 0.548 0.557 0.566 0.577 0.589
BUFFET MARGIN G 2.56 2.56 2.56 2.52 2.48 2.43 2.38 2.33 2.28 2.24
SR NM/LB 0.148 0.15 0.153 0.155 0.158 0.16 0.162 0.165 0.168 0.17
N1 % 71.7 72.4 73.1 73.9 74.7 75.5 76.4 77.3 78 78.8
F FLOW LB/H/ENG 1007 1001 996 992 988 985 983 979 976 975
IAS KT 231 230 229 228 227 226 226 224 223 223
40000 TAS KT 306 310 313 317 321 325 329 333 337 343
INDICATED MACH 0.497 0.504 0.512 0.521 0.529 0.538 0.547 0.556 0.565 0.577
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.53 2.49 2.44 2.38 2.33 2.29
SR NM/LB 0.152 0.155 0.157 0.16 0.163 0.165 0.168 0.17 0.173 0.176
N1 % 70.6 71.2 71.9 72.6 73.3 74.1 75 75.9 76.8 77.6
F FLOW LB/H/ENG 960 953 947 942 937 933 930 928 926 924
IAS KT 227 226 225 224 223 222 221 220 219 218
38000 TAS KT 300 304 307 311 315 318 322 327 331 335
INDICATED MACH 0.488 0.495 0.503 0.511 0.519 0.528 0.537 0.546 0.555 0.564
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.54 2.49 2.44 2.39 2.34
SR NM/LB 0.156 0.159 0.162 0.165 0.168 0.171 0.173 0.176 0.179 0.181
N1 % 69.5 70.1 70.7 71.4 72.1 72.8 73.6 74.4 75.3 76.2
F FLOW LB/H/ENG 914 907 900 895 890 885 881 878 875 873
IAS KT 222 221 220 219 219 218 217 216 215 214
36000 TAS KT 294 298 301 305 309 312 316 320 324 328
INDICATED MACH 0.479 0.486 0.494 0.502 0.51 0.518 0.527 0.535 0.544 0.554
BUFFET MARGIN G 2.56 2.56 2.56 2.56 2.56 2.56 2.55 2.5 2.45 2.4
SR NM/LB 0.161 0.164 0.167 0.17 0.173 0.176 0.179 0.182 0.185 0.188
INCREASE / DECREASE N1% BY 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE FUEL FLOW 1 % PER 5°C ABOVE / BELOW ISA CONDITIONS.
INCREASE / DECREASE TAS BY 5 KT PER 5°C ABOVE / BELOW ISA CONDITIONS.
FOR ANTI-ICE ON:
INCREASE N1 BY 0.6 % AND FUEL FLOW BY 8%.
DECREASE SR BY 9%.